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Page 27

Note:

N o v e m b e r 1 2 - 1 3 , 2 0 1 8 | R o m e , I t a l y

Joint Event on

OF EXCELLENCE

IN INTERNATIONAL

MEETINGS

alliedacademies.com

YEARS

&

CHROMATOGRAPHY AND SEPARATION SCIENCE

World Congress on

SATELLITE AND SPACE MISSIONS

International Conference and Exhibition on

Chromatography 2018 & Satellite 2018

Journal of Chemical Technology and Applications

|

Volume 2

Thomas Drake Miyano, J Chem Tech App 2018, Volume 2

MOON-BASED PLANETARY DEFENSE

CAMPAIGN

Thomas Drake Miyano

Draconis Aerospace Limited Liability Company, USA

T

he Moon is an ideal location to launch intercepting missions to life-threat-

ening and catastrophic asteroids. The effectiveness of the interception

greatly depends on the weight of the spacecraft. Unfortunately, interceptors

launched from the Earth lose more than 98% of their weight by burning the

majority of their onboard fuel and by jettisoning their lower stage structures

before entering a heliocentric orbit. However, if interceptors are launched

from the Moon by a lunar surface accelerator, they can enter a heliocentric

orbit without consuming any onboard fuel or jettisoning any part of the space-

craft. A 5-ton construction package, which consists of robots and industrial

production equipment, would enable mining on the moon and construction of

a 3.5 km-long, 5,000-ton accelerator.

Large asteroid impacts have and will inevitably occur, and it is important to

be prepared to avoid catastrophes, but they may not happen immediately or

even within the next fifty years. The future planetary defense systemmust be

a dual-use system, which continuously provides a secondary benefit to justify

its operation and maintenance costs. When it is not defending the planet, the

Lunar Electromagnetic Interceptor Launch System (LEILAS) can send over

a thousand tons of construction material and fuel annually to the Low Earth

Orbit (LEO) or Earth-Moon Lagrange Point Two (EML-2) to build space sta-

tions and to construct large spacecraft for deep space missions. The paper

has been published via Journal of Space Safety Engineering and available via

https://www.sciencedirect.com/science/article/pii/S2468896717300617.

Thomas Drake Miyano has completed his Masters of

Aerospace Engineering Degree from the Ohio State Uni-

versity, USA, and received additional education In space

systems operation from the Naval Postgraduate School.

He is the officer in charge of CFWP Det AIMD Iwakuni,

commands 140 personnel and direct intermediate Lev-

el aerospace maintenance for Carrier Air Wing Five. He

is a member of the department of Defense’s acquisition

professional community and certified in the field engi-

neering, manufacturing, contracting and program man-

agement.

thomas.drake.miyano@fe.navy.mil

BIOGRAPHY